68A112149-2006: RIB,AIRFOIL.
The RIB,AIRFOIL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 6.600 INCHES NOMINAL IN, overall_length: 17.250 INCHES NOMINAL IN, aircraft_location: WING-FORWARD,MACHINING, material_thickness: 1.125 INCHES NOMINAL IN, aircraft_station_number: XW127.912 TO XW128.877. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-116-1963, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | ALUMINUM ALLOY 2024 |
| overall_width | 6.600 INCHES NOMINAL IN |
| overall_length | 17.250 INCHES NOMINAL IN |
| aircraft_location | WING-FORWARD,MACHINING |
| material_thickness | 1.125 INCHES NOMINAL IN |
| aircraft_station_number | XW127.912 TO XW128.877 |
| aircraft_mission_design_series | F-15A/TF-15A A |
| material_document_and_classification | MMS 149 T851 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-116-1963 |
| AIRCRAFT STATION NUMBER | XW127.912 TO XW128.877 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS 149 T851 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 17.250 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.600 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 1.125 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | WING-FORWARD,MACHINING |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15A/TF-15A A |
No substitute or cross-reference records for this part.